THIS article derives from one of similar title by H. J. Stewart, in which he gave an account of a simple method of dealing with thin aerofoil theory for small angles of incidence by satisfying the usual approximate condition at the boundary of the aerofoil after expanding the slope of the profile in a Fourier series.
Brennan, M.J. and Stevenson, A.C. (1946), "Simplified Two‐Dimensional Aerofoil Theory: A Basic Method of Determining the Profiles of Laminar Flow and High‐Speed Aerofoils", Aircraft Engineering and Aerospace Technology, Vol. 18 No. 6, pp. 182-194. https://doi.org/10.1108/eb031377
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